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Towards locust-inspired gliding wing prototypes for micro aerial vehicle applications

In aviation, gliding is the most economical mode of flight explicitly appreciated by natural fliers. They achieve it by high-performance wing structures evolved over millions of years in nature. Among other prehistoric beings, locust is a perfect example of such natural glider capable of endured tra...

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Autores principales: Isakhani, Hamid, Xiong, Caihua, Chen, Wenbin, Yue, Shigang
Formato: Online Artículo Texto
Lenguaje:English
Publicado: The Royal Society 2021
Materias:
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC8242835/
https://www.ncbi.nlm.nih.gov/pubmed/34234953
http://dx.doi.org/10.1098/rsos.202253
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author Isakhani, Hamid
Xiong, Caihua
Chen, Wenbin
Yue, Shigang
author_facet Isakhani, Hamid
Xiong, Caihua
Chen, Wenbin
Yue, Shigang
author_sort Isakhani, Hamid
collection PubMed
description In aviation, gliding is the most economical mode of flight explicitly appreciated by natural fliers. They achieve it by high-performance wing structures evolved over millions of years in nature. Among other prehistoric beings, locust is a perfect example of such natural glider capable of endured transatlantic flights that could inspire a practical solution to achieve similar capabilities on micro aerial vehicles. An investigation in this study demonstrates the effects of haemolymph on the flexibility of several flying insect wings proving that many species exist with further simplistic yet well-designed wing structures. However, biomimicry of such aerodynamic and structural properties is hindered by the limitations of modern as well as conventional fabrication technologies in terms of availability and precision, respectively. Therefore, here we adopt finite-element analysis to investigate the manufacturing-worthiness of a three-dimensional digitally reconstructed locust wing, and propose novel combinations of economical and readily available manufacturing methods to develop the model into prototypes that are structurally similar to their counterparts in nature while maintaining the optimum gliding ratio previously obtained in the aerodynamic simulations. The former is assessed here via an experimental analysis of the flexural stiffness and maximum deformation rate as EI(s) = 1.34 × 10(−4) Nm(2), EI(c) = 5.67 × 10(−6) Nm(2) and greater than 148.2%, respectively. Ultimately, a comparative study of the mechanical properties reveals the feasibility of each prototype for gliding micro aerial vehicle applications.
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spelling pubmed-82428352021-07-06 Towards locust-inspired gliding wing prototypes for micro aerial vehicle applications Isakhani, Hamid Xiong, Caihua Chen, Wenbin Yue, Shigang R Soc Open Sci Engineering In aviation, gliding is the most economical mode of flight explicitly appreciated by natural fliers. They achieve it by high-performance wing structures evolved over millions of years in nature. Among other prehistoric beings, locust is a perfect example of such natural glider capable of endured transatlantic flights that could inspire a practical solution to achieve similar capabilities on micro aerial vehicles. An investigation in this study demonstrates the effects of haemolymph on the flexibility of several flying insect wings proving that many species exist with further simplistic yet well-designed wing structures. However, biomimicry of such aerodynamic and structural properties is hindered by the limitations of modern as well as conventional fabrication technologies in terms of availability and precision, respectively. Therefore, here we adopt finite-element analysis to investigate the manufacturing-worthiness of a three-dimensional digitally reconstructed locust wing, and propose novel combinations of economical and readily available manufacturing methods to develop the model into prototypes that are structurally similar to their counterparts in nature while maintaining the optimum gliding ratio previously obtained in the aerodynamic simulations. The former is assessed here via an experimental analysis of the flexural stiffness and maximum deformation rate as EI(s) = 1.34 × 10(−4) Nm(2), EI(c) = 5.67 × 10(−6) Nm(2) and greater than 148.2%, respectively. Ultimately, a comparative study of the mechanical properties reveals the feasibility of each prototype for gliding micro aerial vehicle applications. The Royal Society 2021-06-30 /pmc/articles/PMC8242835/ /pubmed/34234953 http://dx.doi.org/10.1098/rsos.202253 Text en © 2021 The Authors. https://creativecommons.org/licenses/by/4.0/Published by the Royal Society under the terms of the Creative Commons Attribution License http://creativecommons.org/licenses/by/4.0/ (https://creativecommons.org/licenses/by/4.0/) , which permits unrestricted use, provided the original author and source are credited.
spellingShingle Engineering
Isakhani, Hamid
Xiong, Caihua
Chen, Wenbin
Yue, Shigang
Towards locust-inspired gliding wing prototypes for micro aerial vehicle applications
title Towards locust-inspired gliding wing prototypes for micro aerial vehicle applications
title_full Towards locust-inspired gliding wing prototypes for micro aerial vehicle applications
title_fullStr Towards locust-inspired gliding wing prototypes for micro aerial vehicle applications
title_full_unstemmed Towards locust-inspired gliding wing prototypes for micro aerial vehicle applications
title_short Towards locust-inspired gliding wing prototypes for micro aerial vehicle applications
title_sort towards locust-inspired gliding wing prototypes for micro aerial vehicle applications
topic Engineering
url https://www.ncbi.nlm.nih.gov/pmc/articles/PMC8242835/
https://www.ncbi.nlm.nih.gov/pubmed/34234953
http://dx.doi.org/10.1098/rsos.202253
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